发明名称 ALUMINUM ALLOY THIN THICKNESS CASTING STRUCTURE FOR AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To provide an aluminum alloy thin thickness casting structure for an aircraft having strength and light weight same as a current structure manufactured by riveting a skin member and a main structure, and having reduced cost by integrating a skin member comprising an aluminum alloy flat plate part and a main structure member comprising a rib, and optimizing the constitution of the reinforcing rib arranged on the skin member. SOLUTION: This aluminum alloy thin thickness casting structure 1 for the aircraft is composed of the skin member 2 comprising the flat plate part composed of high strength aluminum casting alloy; the main structure member X composing the main rib 3 installed in the skin member 2; and the reinforcing rib 4 installed between the main ribs 3. The skin member 2, the main rib 3, and the reinforcing rib 4 are integratedly formed by casting.
申请公布号 JP2002145195(A) 申请公布日期 2002.05.22
申请号 JP20000344825 申请日期 2000.11.13
申请人 KOBE STEEL LTD 发明人 SHIBATA AKINORI;NAKADA MAMORU;KOIKE SUSUMU
分类号 B64C1/12;B64C1/14;(IPC1-7):B64C1/12 主分类号 B64C1/12
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